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Aircraft architecture with a reduced bleed aircraft secondary power system 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64B-001/24
출원번호 US-0076898 (2002-02-14)
발명자 / 주소
  • Albero, Jose
  • Lents, Charles E.
  • Sahm, Michael K.
  • Welch, Richard C.
출원인 / 주소
  • Hamilton Sunstrand Corporation
대리인 / 주소
    Bachman & LaPointe, P.C.
인용정보 피인용 횟수 : 33  인용 특허 : 7

초록

The present invention relates to an improved architecture for an aircraft. The aircraft has a first engine, a first gearbox associated with the first engine, a first starter/generator associated with the gearbox, and a first motor drive connected to the first starter/generator for providing the star

대표청구항

The present invention relates to an improved architecture for an aircraft. The aircraft has a first engine, a first gearbox associated with the first engine, a first starter/generator associated with the gearbox, and a first motor drive connected to the first starter/generator for providing the star

이 특허에 인용된 특허 (7)

  1. Coffinberry George A. (West Chester OH), Aircraft engine electrically powered boundary layer bleed system.
  2. Glennon Timonthy F., Aircraft secondary power system.
  3. Rodgers Colin (San Diego CA), Auxiliary power unit for use in an aircraft.
  4. Sutrina Thomas (Rockford IL) Crowe Lawrence E. (Lindenwood IL) Smith Edward W. (Pecatonica IL) Peterson Ronald F. (Rockford IL) Hoppe Richard J. (Rockford IL), Electric power distribution module for an electric power generation and distribution system.
  5. Jeffrey Ronald Coles GB; Marc Holme GB; James Patrick Doyle GB, Electrical generator an aero-engine including such a generator, and an aircraft including such a generator.
  6. Williams Kenneth R., Multi-mode secondary power unit.
  7. Cronin Michael J. (Sherman Oaks CA), Tandem-generator design for aircraft.

이 특허를 인용한 특허 (33)

  1. Himmelmann, Richard A.; Lang, David, Actuator with differential and brake.
  2. Napier, James C., Air inlet noise attenuation assembly.
  3. Burns, Donald; Rajashekara, Kaushik, Aircraft and propulsion system.
  4. Balan, Chellappa; Sheldon, Karl Edward, Aircraft auxiliary gas turbine engine and method for operating.
  5. Burns, Donald; Rajashekara, Kaushik, Aircraft, propulsion system, and system for taxiing an aircraft.
  6. Burns, Donald; Rajashekara, Kaushik, Aircraft, propulsion system, and system for taxiing an aircraft.
  7. Light, Stacey H.; Vitale, Jack V., Auxiliary power unit inlet.
  8. Light, Stacey H.; Vitale, Jack V., Auxiliary power unit inlet.
  9. Parikh, Pradip G., Combined cabin air and heat exchanger RAM air inlets for aircraft environmental control systems, and associated methods of use.
  10. Fucke, Lars; Daggett, David L., Combined fuel cell aircraft auxiliary power unit and environmental control system.
  11. Fucke,Lars; Daggett,David L., Combined fuel cell aircraft auxiliary power unit and environmental control system.
  12. DeRoy, Robert M., Electric compressor for use with a wing anti-ice system.
  13. Mehl, Byron R.; Baker, Donal, Electric engine start with two motors and single motor drive.
  14. Atkey,Warren A.; Bernier,Alan T.; Bowman,Michael D.; Campbell,Thomas A.; Cruse,Jonathan M.; Fiterman,Charles J.; Meis,Charles S.; Ng,Casey Y. K.; Nozari,Farhad; Zielinski,Edward, Electric-based secondary power system architectures for aircraft.
  15. Shander, Mark S.; Cote, Richard A.; Drake, Michael L.; Carter, III, Howard; Peters, John T.; Ng, Casey Y. K.; Hoag, Michael S.; Paterson, John T., Electrical systems architecture for an aircraft, and related operating methods.
  16. Baumann, Joerg, Emergency ram air inlet valve of an aircraft.
  17. Maddali, Vijay K.; Rozman, Gregory I.; Dooley, Kevin, Engine having power bus fault short circuit control with a disconnection switch.
  18. Francisco, Jay M.; Napier, James C., Exhaust silencer with baffles.
  19. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin, Independent power generation in aircraft.
  20. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin, Independent power generation in aircraft.
  21. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M., Integrated environmental control and auxiliary power system for an aircraft.
  22. Brighton, Trevor Anthony; Elms, Martin John; Jones, Maxwell William, Landing gear.
  23. Bernard,Guy, Method and apparatus for inhibiting accretion of airborne material on a surface of an aircraft.
  24. Francisco, Jay M.; Napier, James C.; Sapiro, Dan G.; Hagshenas, Behzad, Mixed-flow exhaust silencer assembly.
  25. Maier, Josef; Beutel, Michael, Power distribution architecture for aircraft.
  26. Mehrer, Michael E.; Spencer, John P.; Vaziri, Massoud, Power distribution system and load management protocol therefor.
  27. Derouineau, Jean-Luc; Pearson, Wayne T.; Jonqueres, Michel A., Smart hybrid electric and bleed architecture.
  28. Sheldon, Karl Edward; Turco, John, System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine.
  29. Berenger,Serge, System for powering and controlling electrical equipment of an aircraft engine or its environment.
  30. Space, David R.; Matera, Jane V.; Atkey, Warren A.; Fiterman, Charles J.; Gray, John; Arnaud, Timothy J., Systems and methods for providing airflow in an aerospace vehicle.
  31. Zielinski, Edward; Bernier, Alan T.; Knechtel, Kent W.; Campbell, Thomas A.; White, Jeffrey J.; Ralston, Mark D., Systems and methods for starting aircraft engines.
  32. Bovitz, David J., Universal AC or DC aircraft device power supply having power factor correction.
  33. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny), Vehicle electrical power management and distribution.
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